This AD revises EASA AD 2019-0237-E dated 20 September 2019. This AD is revised to remove the references to the TN instruction paragraphs, which have changed with TN issue 01.b. The revised TN issues were added to the list of reference publications.

Correction

Not applicable

Supersedure

None

Publication(s) and related information

DG-Flugzeugbau GmbH TN1000/42 and TN500/13 (single document), original issue (01.a) dated 18 July 2019 or Issue 01.b dated 11 September 2019. (German version TM1000/42 and TM500/13 original issue 01.a dated 17 July 2019 or issue 01.b dated 11 September 2019).
DG-Flugzeugbau GmbH RI-DG-05 original issue dated 15 August 2019 (German version RA_DG-05 dated 15 August 2019).
The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD

Remarks

1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD.
2. The results of the safety assessment have indicated the need for immediate publication and notification, without the full consultation process.
3. Enquiries regarding this AD should be referred to the the EASA Programming and Continued Airworthiness Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.
4. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system.

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